• 제목/요약/키워드: combustion zone

검색결과 386건 처리시간 0.022초

디젤기관에서의 경유-메탄올 혼합유의 연소 안전성과 연소특성에 관한 연구 (A Study on the Combustion Stability and Characteristics for D.O - Methanol Blending Oil in Diesel Engine)

  • 김상암;왕우경
    • 동력기계공학회지
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    • 제22권1호
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    • pp.48-55
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    • 2018
  • It has recently been reported that methanol fuel has been used in the product carrier with established duel fuel engine, which has been greatly reducing emissions of $CO_2$, NOx and SOx from the engine. However, to use methanol alone as fuel oil in a general diesel engine, design modification of cylinder head is needed because the ignition aid device or the duel fuel injection system is needed. On the other hand, only if the mixer is installed on the fuel oil supply line, diesel oil - methanol blending oil can be used as fuel oil for the diesel engine, but there is a problem of the phase separation when two fuels are mixed. In this study, diesel oil and methanol were blended compulsorily in preventing the phase separation with installing agitators and a fuel oil boost pump on fuel line of a test engine. Also, cylinder pressure and fuel consumption quantity were measured according to engine load and methanol blending ratio, and indicated mean effective pressure, heat release rate and combustion temperature obtained from the single zone combustion model were analyzed to investigate the effects of latent heat of vaporization of methanol on combustion stability and characteristics. As a result, the combustion stability and characteristics of 10% methanol blending oil are closest to the those of diesel oil, and it could be used as fuel oil in existing diesel engines without deterioration of engine performance and combustion characteristics.

연료노즐 출구에서의 속도 형상에 따른 부상화염 높이 및 화염구조에 관한 수치해석 연구 (A Numerical Analysis of Flame Liftoff Height and Structure with the Variation of Velocity Profiles at the Nozzle Exit)

  • 하지수;김태권;박정
    • 한국가스학회지
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    • 제12권4호
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    • pp.21-28
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    • 2008
  • 삼지화염과 포와젤(Poiseuille) 및 균일분포 연료출구 속도에 따른 부상화염의 부상거동 그리고 화염면 부근에서의 연소 유동 특성에 대하여 수치적 해석을 수행하였다. 부상화염에 대한 수치해석으로 기존 연구 결과를 검정하고 화염대 부근에서 구조적 특성을 살펴보며 포와젤 및 균일분포 연료출구속도 조건에서 운동량 유속으로 부상높이를 일반화하여 비교하였다. 또한 화염면 부근에서 속도, 압력, 온도, 화학반응속도 등으로 연소 유동 특성을 분석하고 규명하였다. 특히 중심선을 따른 속도 변화의 경우 노즐에서 화염대 부근까지는 전형적인 비반응제트 유동에 따른 속도 분포를 형성하지만 화염대 직전에서 속도가 급격히 감소하다가 화염대를 지나면서 급격히 증가한 후에 다시 감소하는 현상을 규명하였다. 화염대 전의 유동영역에서는 화염대가 장애물역할을 하다가 화염대를 지나고 나면 유동을 가속시켜주는 역할을 하고 있기 때문이다. 이러한 현상은 기존의 비반응 제트 유동으로 규명하지 못하였던 것이다.

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20kW급 마이크로터빈용 저공해 연소기의 고압고온 성능실험 연구 (An Experimental Study on Low Nox Combustor Performance at High Pressure and Temperature for 20kW Class Microturbines)

  • 윤정중;오종식;이헌석
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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    • pp.183-190
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    • 2002
  • In order to reduce NOx emissions in the 20kw class microturbines under development, the low NOx characteristics, as being an application to the lean premixed combustion technology, have been investigated. The study has been conducted at the conditions of high temperature and pressure. Air from a compressor with the temperature of 500K to 650K and the pressure of 0.3bar gauge to 0.7bar gauge, was supplied to the combustor through an air preheat-treatment. Sampling exhaust gases were measured at the immediate exit of the combustor. for the effect of temperature on NO and CO emissions. though NOx was increased, CO was decreased with increasing inlet air temperature. With increasing inlet air pressure, NOx and CO were increased also. NOx was decreased, but CO was increased with increasing inlet air mass flow rate. The test has been performed on the equivalent ratios of 0.10 to 0.25 in a lean region. NOx was increased with increasing equivalent ratios, but CO was decreased as an influence of flame temperature. In the very lean region of the equivalent ratio below 0.12, CO was increased suddenly, due to instability. As the results of this study, NOx and CO are found to be reduced to the similar level at the same time when operated at optimal conditions.

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직분식 디젤엔진에서 EGR이 연소특성 및 배출가스에 미치는 영향에 대한 시뮬레이션 연구 (Engine Cycle Simulation for the Effects of EGR on Combustion and Emissions in a DI Diesel Engine)

  • 함윤영;전광민
    • 한국자동차공학회논문집
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    • 제10권4호
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    • pp.51-59
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    • 2002
  • In this study, cycle simulation was performed to investigate the effect of EGR on combustion characteristics and emissions including NO and soot using a two-zone model in a DI diesel engine. The NO formation was well predicted for different EGR rate and temperature using a two-zone model. The oxygen in the inlet charge was replaced by CO$_2$ and H$_2$O with EGR. The reduction in the inlet charge oxygen resulted in very large reduction in NO level at the same inlet charge temperature. The effect of EGR was to reduce the burned gas temperature. When EGR was increased from 0% to 15%, the peak flame temperature was decreased by 50$\^{C}$ and it caused about 57% NO reduction. EGR caused increase of the overall inlet charge temperature which offset some of benefit of lower flame temperature resulting from O$_2$ displacement. Cooling the EGR was confirmed to provide additional benefits by lowering NO emission. It also reduced soot emission.

Non-premixed Hydrogen Flame Structure in Supersonic Coflowing Air Flows

  • Kim, Ji-Ho;Kim, Je-Hung;Yoon, Young-Bin;Park, Chul-Woung;Hahn, Jae-Won
    • 한국연소학회지
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    • 제7권1호
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    • pp.1-7
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    • 2002
  • Experiments have been performed to investigate the structure of axisymmetric hydrogen diffusion flame in a supersonic coflow air. The characteristics and structure of supersonic flames are compared with those of subsonic flames as the velocity of coflow air increases from subsonic to supersonic velocity of Mach 1.8. Also, the subsonic and supersonic flow fields are analyzed numerically for the non-reacting conditions and the possible flame contours indicated by fuel mass fraction are compared with the measured OH radical distributions. It is found that the flame structure indicates more like a partially premixed flame as the coflow air velocity is increased from subsonic to supersonic regimes; strong reaction zone indicated by intense OH signal is found at the center, which is different from subsonic flame cases. And it is shown that the fuel jet passes along the recirculation zones behind the bluff-body fuel nozzle resulting in relatively long mixing time. This is believed to be the reason of the partially premixed flame characteristics found in the present supersonic flames.

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동축 수소 확산화염에서의 NOx 생성 분석 (Analysis of NOx Emissions in Thrbulent Nonpremixed Hydrogen-Air Jet Flames with Coaxial Air)

  • 박양호;김성룡;문희장;윤영빈;정인석
    • 한국연소학회지
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    • 제5권1호
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    • pp.19-30
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    • 2000
  • The characteristics of NOx emissions in pure hydrogen nonpremixed flames with coaxial air are analyzed numerically for the three model cases of coaxial air flames classified by varying coaxial air velocity and/or fuel velocity. In coaxial air flames, the flame length is reduced by coaxial air and can be represented as a function of the ratio of coaxial air to fuel velocity. Coaxial air decreases flame reaction zone, resulting in reducing flame residence time significantly. Finally, the large reduction of EINOx is achieved by the decrease of the flame residence time. It is found that because coaxial air can break down the flame self-similarity law, appropriate scaling parameters, which are different from those in the simple jet flames, are recommended. In coaxial air flames, the flame residence time based on the flame volume produces better results than that based on a cube of the flame length. And some portion of deviations from the 1/2 scaling law by coaxial air may be due to the violation of the linear relationship between the flame volume and the flame reaction zone.

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노크이론 확립을 위한 말단가스 온도 및 압력 경과이력 (A study on the development of temperature and pressure at the end-gas zone during the combustion period to establish the knock theory)

  • 이성열;오영일
    • 오토저널
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    • 제15권1호
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    • pp.28-36
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    • 1993
  • Present-day there are two of theories which have considerable scientific support to explain the knock phenomenon in S.I. engine, the detonation theory and the autoignition theory. But they still have some problems to explain effects of knock parameters, i.e.. compression ratio, spark timing, mixture quality, engine speed, ect, on knocking process in S.I. engine. Accordingly, it is essential to find out whish is more adequate theory of two and to develop the method of analyzing knock phenomenon, that is the aim of this paper. The Authors develop the method of predicting transient temperature and pressure at the end-gas zone during the combustion period and analyze knocking process by this method based on the knock theories. The caluculated values based on the autoignition theory show reasonablly correct relations between knock parameters and knock process but there is no evidence of knock occurred by detonation theory through the calculation according to the all parameters. The authors find out that the autoignition theory is more adequate than detonation theory to analyze knocking process in S.I. engine.

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IDI 디젤기관의 단일영역 열발생량 계산 (One-zone heat release analysis for IDI diesel engine)

  • 이석영;김규보;최승환;전충환;장영준;전광민
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.830-836
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    • 2001
  • An one-zone heat release analysis was studied for a 4 cylinder indirect diesel engine. The object of the study is to calculate the heat release accurately including the effect of specific heat ratio, heat transfer and crevice volume and to find out combustion characteristics of an indirect diesel engine cosidering the effect of both pressure in the main and swirl chambers. The integrated gross heat release values were close to the measured fuel energy at various full load operating conditions.

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6기통 압축착화 기관의 단일 영역 열방출량 계산 (An One-zone Heat Release Analysis of a 6 Cylinder Compression-Ignition Engine)

  • 신범식;이석영;전광민
    • 한국자동차공학회논문집
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    • 제4권1호
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    • pp.147-154
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    • 1996
  • An one-zone heat release analysis was studied for a 6 cylinder direct injetction compressionignition engine. The heat transfer constants in this anlysis were calibrated to match the measured fuel energy at 1,000 rpm full load, which was the fuel mass multiplied by the fuel's heating value. The integrated gross heat release values were close to the measured fuel energy at various full load operating conditions. The combustion inefficiency from this calculation was proportional to the smoke of exhaust gas.

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소규모 반응로를 이용한 감압 잔사유지 연소실험 (The Experimental Studies of Vacuum Residue Combustion in a Small Scale Reactor)

  • 박호영;김영주;김태형;서상일
    • 에너지공학
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    • 제14권4호
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    • pp.268-276
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    • 2005
  • 액체연료(중유)공급량 기준 20kg/hr규모의 반응로에서 증기분무 내부 혼합식 노즐을 이용하여 잔사유의 연소실험을 수행하였다. 본 실험에서 사용한 감압 잔사유는 점도가 높고 황함량, 잔류탄소와 금속성분의 함량도 높았다. 잔사유의 착화를 위해서는 반응로를 일정온도까지 예열하여야 했으며 이는 LPG를 이용하였다. 잔사유 공급량을 변화시키면서 축방향 및 반경방향의 로내 가스 온도, 주요 가스농도 및 채집된 고체 입자를 분석하였다. 잔사유의 주반응영역은 버너 팁으로부터 약 1 m 근방에서 형성되었으며 이는 축방향 가스 온도, 농도 분포 및 입자의 크기로부터 확인할 수 있었고, 반응로의 하류에서는 완전 확립된 온도분포를 보여주고 있었다. 고체 입자의 SEM 분석으로부터 잔류 탄소입자는 기공이 많은 형태를 띠고 있었다.